R.530
R.530
Air-to-air missile. Year: 1963. IOC: 1963. Country: France.

Manufacturer: Matra. Liftoff Thrust: 83.300 kN (18,727 lbf). Total Mass: 195 kg (429 lb). Core Diameter: 0.27 m (0.88 ft). Total Length: 3.29 m (10.79 ft). Span: 1.10 m (3.60 ft). Standard warhead mass: 27 kg (59 lb). Maximum range: 18 km (11 mi). Boost Propulsion: Solid rocket. Guidance: Infrared or Semi-Active Radar Homing. Total Number Built: 4000. Flyaway Unit Cost $: 0.044 million.


 
 
 
 
 
 
 
 
 

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